CN103016143B - Novel internal-combustion engine - Google Patents

Abstract

The invention provides a technical scheme of a novel internal-combustion engine. The technical scheme of the novel internal-combustion engine is a technical scheme of a multi-fuel internal-combustion engine and includes that the internal-combustion engine comprises pressurizing rotors, acting rotors, a combustion chamber, a fuel supply device and an igniter. Each pressurizing rotor can be a pressurizing mechanism with one, two or more than two or multi-stage mixed stage. Each acting rotor is of non-turbine type impeller structure, a tongue sheet capable of moving vertically and identical with vanes in width is arranged between two adjacent vanes of the acting rotors, the cylindrical combustion chamber is provided with a cylindrical piston matched with an inner ring of the combustion chamber, the center of the piston is provided with an air spraying hole, a fuel sprayer is mounted in the air spraying hole, a piston position controller is arranged at the rear end of the piston, exhaust quantity/circle, volume of the combustion chamber of the internal-combustion engine can be variable, controllable and adjustable by controlling the tongue sheets and the piston in the combustion chamber.

Description

A kind of internal combustion engine

technical field:

What the present invention relates to is a kind of motor, especially a kind of explosive motor.

background technique:

In the prior art, the technology the most close with the application is gas turbine, its rotating speed accommodation of gas turbine of the single acting rotor that combustion pressure is coaxial is narrower, the rotating ratio of calming the anger between rotor and acting rotor is immutable, on the gas turbine of multiple rotor that freely does work, its multiple rotor that freely does work is in a blast tube, still by flow restriction, it restricts multiple rotating speed freely done work between rotor mutually, make to calm the anger the compression ratio of rotor output squeezing air or flow control scope relative narrower, although split gas turbine and axial flow gas engine have been accomplished to fire pressure split axle, but it is calmed the anger, acting rotor and power stage acting rotor still coexist in a blast tube, its acting rotor of calming the anger when tick-over still restricts by it, cannot accomplish that high low speed adapts to mutually, make its power stage scope and operating mode accommodation relative narrower, in prior art, the acting rotor of gas turbine is all almost turbine or the page wheel of turbine-type besides, its shape, week/air displacement immobilizes all relatively, its air displacement of doing work rotor under identical operating air pressure is immobilized relatively, the problem place that during Here it is gas turbine low speed, oil consumption is higher, can not use at low speeds, be exactly the size of its puff prot in addition, the shape of firing chamber, volume immobilizes, make fuel from injection, mixing, igniting, the distance being burned to acting rotor all immobilizes, make fuel Applicable scope relative narrower, pluralities of fuel can not be used, the deficiency that Here it is existing for prior art.

summary of the invention:

Technical problem to be solved by this invention, be exactly for the deficiency existing for prior art, and provide a kind of do work rotor at the same pressure week/shape of air displacement and firing chamber and do work rotor and all adjustable variable controllable of rotating ratio of calming the anger between rotor, its rotating speed Applicable scope is wider, power stage wider range, can working, can realize the technological scheme that multi fuel exchanges when not changing machine hardware under complex working conditions.

This programme is achieved by the following technical measures: primarily of body, to calm the anger rotor, acting rotor, firing chamber and fuel supplying device and ignition mechanism are formed, described rotor of calming the anger is arranged in body chamber with acting rotor, described body chamber can be circle also can be oval, described depressor rotor is with doing work rotor on same axis, acting rotor and calm the anger between rotor and have interval body wall, spring bearing is had in body wall, porting and firing chamber and various pipeline is had in body wall, described rotor of calming the anger can be the various forms of gas pressure mechanisms being applicable to this programme in prior art, as centrifugal turbocompressor, blade pump type gas compressor or turbine-type hinge gas compressor etc., described rotor of calming the anger can be the single-stage be made up of single rotor of calming the anger structure of calming the anger also can be two-stage that two rotors of calming the anger are formed structure of calming the anger can also be the multistage compressor structure that multiple rotor of calming the anger is formed, as multistage turbine gas compressor, multistage blade gas compressor etc., described rotor of calming the anger can also be the hybrid multi-stage gas pressure mechanism that the gas compressor of various ways is formed, be final stage as made primary centrifugal turbocompressor with turbine hinge formula gas compressor, centrifugal turbocompressor is primary blades pump type gas compressor is the mixed construction such as middle final stage, described multistage compressor structure or hybrid multi-stage gas pressure mechanism at different levels between can be coaxial pattern also can be by the split axle pattern that planetary gear set connects can also be that selectively to use planetary gear set to carry out connection coaxial, split axle is used with, specifically can select integrated mode flexibly according to actual needs, described planetary gear set there is planetary gear set control gear, described planetary gear set control gear can lock wantonly two gears in planetary gear set also locking or control can be in that gear of free state, described acting rotor can be single acting rotor also can be two acting rotors or the multiple acting rotor of two or more, when described acting rotor is two, it can coaxial connection can also be also connect through planetary gear set that two acting rotor shafts can not connect, when described acting rotor is multiple, first acting rotor also can also connect by planetary gear set with not connecting between the second acting rotor in coaxial connection, with coaxial, other acting rotor can connect that also can to connect by planetary gear set can also be selectively use planetary gear set or axle to connect, described acting rotor be two or more multiple time, two acting rotors or multiple acting rotor can share a firing chamber or not share a firing chamber, can also selectively divide into groups combustion chamber shared, described acting rotor shaft and to calm the anger between rotor shaft can be coaxial connection also can be connect through planetary gear set, described acting rotor is non-turbine-type blade wheel structure, described impeller can be unshrouded impeller also can be blade while be all made up of the double shrouded wheel of wheel sheet shutoff the single shrouded wheel or blade both sides of taking turns sheet shutoff, blade on described impeller also can not can contact with body chamber wall with the contact of body chamber wall, blade on described impeller can be the stator blade be fixed on wheel body, described fixed blade can tilt also can tilt counterclockwise in the past clockwise in the past.Have with blade with wide and can be up and down tongue piece between adjacent two blades on described impeller, a limit of described tongue piece is carried out activity with a blade top margin in adjacent two blades with movable axis and is connected, described movable axis can also can on the clockwise side top margin of blade on the counterclockwise side top margin of blade, described tongue piece is that the blade face of another edge, axle center another blade adjacent slides up and down within the scope of 90 degree with coupling shaft, its top dead center is no more than corresponding blade top margin, its radian of blade face camber corresponding to described tongue piece active edges and the slip radian of tongue piece sliding edge match, in unshrouded impeller structure when tongue piece sliding edge is at top dead center adjacent two blades, tongue piece, the rotor cavity of an opposing seal is formed between wheel body and acting rotary piston machine body cavity two wall.Blade on described impeller also can be mounted in the movable blade in wheel body axial notch, described blade tip face can have with blade with wide axial blade groove, roller is had to follow the contact of oval acting rotor chamber inner headed face in described vane groove, acting rotary piston machine housing sidewalls have with annular gas tank corresponding bottom axial notch, communicate with the annular gas tank on acting rotary piston machine housing sidewalls bottom axial notch, described movable blade can slide from inside to outside in axial notch, described blade interior edge face can there is spring bottom axial notch, vane hole is had in described blade, have with blade with wide and can be up and down tongue piece between adjacent two blades on described impeller, described tongue piece inserts by tongue piece convex body and tongue piece concave volume string the scalable tongue piece formed, described tongue piece concave volume internal tongue convex body top end there is spring, a limit of described tongue piece is carried out activity with a blade top margin in adjacent two blades with movable axis and is connected, a limit of described tongue piece fillet can be a limit of tongue piece convex body also can be tongue piece concave volume, described movable axis can also can on the clockwise side top margin of blade on the counterclockwise side top margin of blade, described tongue piece is that the blade face of another edge, axle center another blade adjacent slides up and down within the scope of 90 degree with coupling shaft, its top dead center is no more than corresponding blade top margin, its radian of blade face camber corresponding to described tongue piece active edges and the slip radian of tongue piece sliding edge match, in unshrouded impeller structure when tongue piece sliding edge is at top dead center adjacent two blades, scalable tongue piece, the rotor cavity of an opposing seal is formed between wheel body and acting rotary piston machine body cavity two wall, described rotor cavity communicates with bottom axial notch through vane hole, in double shrouded wheel structure when tongue piece sliding edge is at top dead center adjacent two blades, scalable tongue piece, the rotor cavity of an opposing seal is formed between wheel body and blade two side wheel sheet, axial notch bottom wheel sheet there is corresponding annular gas tank on vent and acting rotary piston machine housing sidewalls communicate, in semi-closed type impeller structure, adjacent two blades when tongue piece active edges is at top dead center, scalable tongue piece, the impeller cavity of an opposing seal is formed between the wheel chamber sidewall of wheel body and blade wheel sheet on one side and blade another side, when blade shutoff side correspondence annular gas tank on one side time, blade shutoff side shaft has corresponding annular gas tank on vent and acting rotary piston machine housing sidewalls to communicate on bottom portion of groove wheel sheet, described annular gas tank communicates with acting rotor air outlet through air flue hole, spring can be had in rotor cavity below described tongue piece, throat less chamber is had in described body, described throat less chamber is on acting rotor chamber, the cylindrical piston matched with firing chamber inner circle is had in described firing chamber, described cylindrical piston is divided into former and later two chambers firing chamber, cylindrical piston can slide in the front and back chamber of firing chamber, described cylindrical piston periphery there is sealed piston ring, there is fumarole at described cylindrical piston center, described fumarole can there is guiding piece also can have guiding groove, in described fumarole, fuel injector is installed, described fuel injector in fumarole can antero posterior axis to activity, described fuel injector in fumarole during front position the aperture of fumarole minimum, described fuel injector in fumarole during rearmost position the aperture of fumarole maximum, spring is had in described cylindrical piston rear end firing chamber rear chamber, described spring rear end has piston position controller, described piston position controller can promote spring or pull spring to come control piston position residing in firing chamber, telescopic pipe is had in described spring ring, described telescopic pipe front end is connected on fuel injector and communicates with fuel injector, telescopic pipe rear end is through piston position controller, body communicates with body outer fuel supplier, control the aperture size of fumarole by the position of telescopic pipe fuel metering sparger in fumarole and then control the spray air flow of fumarole, described firing chamber rear chamber rear end is communicated with rotor air outlet of calming the anger, described firing chamber front chamber front end is communicated with acting rotor suction port, described acting rotor suction port is provided with igniter, described fuel supplying device can be the fuel-supplying unit that can supply various liquid fuel and gaseous fuel being applicable to this programme in prior art, described fuel injector can be applicable to the fuel nozzle that can spray various gas and liquid fuel of this programme or shower nozzle or other fuel injector part in prior art, described ignition mechanism can be the various ignition devices that can be used for this programme in prior art.The concrete feature of this programme also has, described rotor air outlet of calming the anger there is gas storage control valve connect with the outer caisson of body, described caisson can be applicable to the various of this programme in prior art can the gas storage equipment of storing compressed air, described gas storage control valve can make rotor air outlet of calming the anger, firing chamber rear chamber and caisson three intercommunication, gas storage control valve can also close rotor air outlet of calming the anger makes caisson communicate with firing chamber rear chamber separately, gas storage control valve can also be closed the caisson rotor air outlet that makes to calm the anger and be communicated separately with firing chamber rear chamber, in described firing chamber front chamber, there is flameholder at acting rotor suction port place, described flameholder is that the bell gas flow rate that to make in flameholder of porous is lower than the outer gas flow rate of flameholder, make the burning of inflammable mixture more stable, there is rotatable cam axle at acting rotor suction port place, acting rotor suction port can be closed or open to described camshaft, the aperture size of acting rotor suction port can be regulated by camshaft, control gas flow and the direction of acting rotor suction port, the air flue that on described acting rotor chamber sidewall, annular gas tank follows acting rotor air outlet to communicate there is air valve, described air valve has two-way pneumatic control function, air-flow in air flue can be made air-flow in air flue also can only to be made can only can also to make air-flow two-way flow in air flue toward another side flowing toward while flow, the outer air outlet flue of gas port that described acting rotor air outlet follows annular gas tank to communicate there is gas exhausting valve, exhaust pressure and the air displacement at acting rotor air outlet place can be regulated and controled by gas exhausting valve, described gas storage control valve, air valve, gas exhausting valve, fuel injector, piston position controller and planetary gear set control gear can be all the electric controller or the electrical apparatus element such as electric control mechanism and electronic control device that can be used for this programme in prior art.

The beneficial effect of this programme can be learnt according to describing of such scheme, due in this scenario one: have piston in firing chamber, in work, piston automatically can regulate relative position residing between chamber before and after in firing chamber under the interaction of compressed air pressure forward and gaseous-pressure backward and spring according to different operating condition, can also spring be promoted by piston position controller or pull the position of spring to piston to adjust, as: when use hydrogen, liquid gas, rock gas, during the gaseous fuels such as coal gas, due to the diffusivity of gaseous fuel, flammability is all relatively the highest, the front position that spring handle piston is pushed into forward firing chamber front chamber can be promoted with piston position controller, make firing chamber front chamber inner capacities relatively little, when use gasoline, light kerosene, during the volatile liquid fuel such as alcohol, due to the diffusivity of this class A fuel A, flammability is higher, spring can be pulled piston to be adjusted back to relative middle section position before and after in firing chamber between chamber with piston position controller, when use kerosene, during the not volatile heavy class A fuel A such as diesel oil, spring can be pulled piston to be adjusted back in firing chamber in rear chamber position rearward with piston position controller, make firing chamber front chamber length relatively the longest, extend fuel from injection, be mixed into the distance of burning, relative prolongation fuel is done time in advance with compressed-air actuated, also have, pressurized air in the rear chamber of firing chamber is when fumarole sprays into firing chamber front chamber, under the guide functions of pressurized air guiding piece and guiding groove in fumarole by several angle helically eddy current spray into firing chamber front chamber, extend fuel relatively further from injection, be mixed into the distance of burning, extend fuel relatively further and improve mixture homogeneity diffusion time, make fuel combustion more abundant.Realize firing chamber variable adjustable controlled fuel Applicable scope is become wider.Two: the blade of acting rotor has tongue piece, described tongue piece is at outside exhaust gas pressure, can automatically carry out according to different operating mode the sliding position that regulates on blade under the interaction of centrifugal force and inside acting gaseous-pressure, reach automatically regulate acting rotor week/air displacement, air valve on the air flue that can also be communicated with acting rotor air outlet by annular gas tank on the gas exhausting valve on the outer air outlet flue in acting rotor air outlet and the described acting rotor chamber sidewall relative position controlled on blade face that gas pressure in rotor cavity and then adjustment tongue piece slide in correspondence regulate and control to do work rotor week/air displacement, make acting rotor week/air displacement realizes variable adjustable controlled.Three: at acting rotor with to calm the anger between rotor and acting rotor and acting rotor, the rotor and calming the anger between rotor of calming the anger connects by planetary gear set, because planetary gear set is a kind of special gear structure, its structural type is changeable can choice structure pattern be made acting rotor and calm the anger between rotor automatically to adjust rotating ratio according to various working condition at work arbitrarily, allow acting rotor and calm the anger between rotor and accomplish self adaption, the rotating ratio that can also carry out adjustment acting rotor by planetary gear set control gear and calm the anger between rotor, the rotor that makes to calm the anger can export the pressurized air of different compression ratio under identical acting rotor speed condition, realize the variable adjustable controlled of compression ratio, different pressurized gas pressure required for multifuel firing can be provided under the condition not changing machine hardware, realize a machine multi fuel.Four: the fumarole aperture that can be adjusted inner carrier center, firing chamber as required by fuel injector, regulate compression gas blowout flow of the people, realize fuel, pressurized gas is two-way adjustable, the bell flameholder of porous can make part inflammable mixture flow velocity low relative to the outer inflammable mixture flow velocity of flameholder, make combustion gas can smooth combustion under high flow rate, by the gas flow rate at camshaft adjustable acting rotor suction port place and gas flow and direction.Five: when starting the machine, gas storage control valve is closed rotor air outlet of calming the anger and is opened caisson, caisson compressed air enters firing chamber front chamber through firing chamber rear chamber and opens with closing caisson after fuel mix ignition startup acting rotor turns rotor suction port of calming the anger, what startup was become is simple, reliably, easy to operate, gas storage control valve can also open the excess compressed air that caisson is used in storage work as required, discharge again when needing extra reinforcing to use and reach energy-conservation object, six: when acting rotor is multiple, can can selectively use or stop one or several acting rotor according to operating mode to the requirement of output power, what power stage scope and accommodation were become is wider.In sum, the technical program has higher adaptive response and wider modification scope and simple to operationly also can realize multi fuel under complex working conditions, the operation of full electronic control technology can be realized, be particularly suitable for the power platform exploitation of computer programming intelligent control system.As can be seen here, the technical program compared with prior art, has novelty, substantive distinguishing features and remarkable progress, and its beneficial effect implemented also is apparent.

accompanying drawing illustrates:

Fig. 1 is the structural representation of this programme first embodiment.

Fig. 2 is along A place line cross cut structure schematic diagram in Fig. 1.

Fig. 3 is B place enlarged view in Fig. 2.

Fig. 4 is the structural representation of this programme second embodiment.

Fig. 5 is along A place line cross cut structure schematic diagram in Fig. 4.

Fig. 6 is the structural representation of this programme the 3rd embodiment.

Fig. 7 is along A place line cross cut structure schematic diagram in Fig. 6.

Fig. 8 is the structural representation of this programme the 4th embodiment.

Fig. 9 is along A place line cross cut structure schematic diagram in Fig. 8.

Figure 10 is C place enlarged view in Fig. 9.

Figure 11 is the structural representation of this programme the 5th embodiment.

Figure 12 is perspective structure schematic diagram before Figure 11.

Figure 13 looks sectional structure schematic diagram under the end face of Figure 11.

Figure 14 is the structural representation of this programme the 6th embodiment.

Figure 15 is along A place line cross cut structure schematic diagram in Figure 14.

Figure 16 looks sectional structure schematic diagram under Figure 14 end face.

Figure 17 is the structural representation of this programme the 7th embodiment.

Figure 18 is A place line plane of structure perspective structure schematic diagram in Figure 17.

Figure 19 is the structural representation of this programme the 8th embodiment.

Figure 20 is along A place line cross cut structure schematic diagram in Figure 19, Figure 21, Figure 22, Figure 23, Figure 24, Figure 25.

Figure 21 is the structural representation of this programme the 9th embodiment.

Figure 22 is the structural representation of this programme the tenth embodiment.

Figure 23 is the structural representation of this programme the 11 embodiment.

Figure 24 is the structural representation of this programme the 12 embodiment.

Figure 25 is the structural representation of this programme the 13 embodiment.

In figure, 1 is body, 2 is centrifugal rotor of calming the anger, 3 is acting rotor, 3 ' is the second acting rotor, 3 〞 are the 3rd acting rotor, 4 is rotor suction port of calming the anger, 5 is rotor shaft of calming the anger, 6 is acting rotor shaft, 6 ' is the second acting rotor shaft, 6 〞 are the 3rd acting rotor shaft, 7 is bearing, 8 is piston, 9 is piston ring, 10 is firing chamber front chamber, 10 ' is the second firing chamber front chamber, 11 is firing chamber rear chamber, 11 ' is the second firing chamber rear chamber, 12 is fumarole, 13 is fuel injector, 14 is spring, 15 is piston position controller, 16 is telescopic pipe, 17 is fuel supplying device, 18 is rotor air outlet of calming the anger, 19 is gas storage valve, 20 is caisson, 21 is acting rotor suction port, 21 ' second acting rotor suction port, 21 〞 are the 3rd acting rotor suction port, 22 is ignition mechanism, 23 is flameholder, 24 is camshaft, 25 acting rotor air outlets, 25 ' is the second acting rotor air outlet, 25 〞 are the 3rd acting rotor air outlet, 26 is air outlet flue, 26 ' is second row air flue, 27 is guiding piece, 28 is blade, 29 is axial notch, 30 is groove spring, 31 is wheel sheet, 32 is planetary gear set, 33 planetary gear set control gear, 34 is annular gas tank, 35 is vent, 36 is air flue, 36 ' is the second air flue, 36 〞 are the 3rd air flue, 37 is air valve, 38 is gas exhausting valve, 39 is tongue piece, 40 is movable axis, 41 is rotor cavity, 42 is vane groove, 43 is roller, 44 is tongue piece concave volume, 45 is tongue piece convex body, 46 is tongue piece spring, 47 is vane hole, 48 is bull gear, 49 is planetary carrier, 50 is sun gear, 51 to calm the anger rotor for blade pump type, 52 to calm the anger rotor for previous stage blade pump type, 53 to calm the anger rotor suction port for previous stage, 54 to calm the anger rotor air outlet for previous stage, 55 to calm the anger rotor shaft for previous stage, 56 to calm the anger rotor for turbine-type, 56 ' to calm the anger rotor for previous stage turbine-type, 56 〞 are that front secondary turbine-type is calmed the anger rotor, 57 to calm the anger rotor shaft for front secondary, 58 to calm the anger rotor air outlet for front secondary, 59 to calm the anger rotor suction port for front secondary, 60 to calm the anger rotor shaft for first three level, 61 to calm the anger rotor suction port for first three level, 62 to calm the anger rotor air outlet for first three level, 63 to calm the anger rotor shaft for front level Four, 64 to calm the anger rotor suction port for front level Four, 65 to calm the anger rotor air outlet for front level Four.

embodiment:

For the technical characterstic of this programme more can be clearly demonstrated, below by 13 embodiments, and in conjunction with its accompanying drawing, this programme is further elaborated.

Fig. 1, Fig. 2, Fig. 3 collectively illustrates this programme first embodiment, can be found out by accompanying drawing, internal combustion engine shown in the present embodiment is by body 1, centrifugal calm the anger rotor 2 and non-turbine-type acting rotor 3 form, described rotor 2 of calming the anger same axis is arranged on respectively cylindrical shape in body 1 with acting rotor 3 and calms the anger in rotor 2 chamber and acting rotor 3 chamber, described rotor 2 of calming the anger is contained in calms the anger on rotor shaft 5, described acting rotor 3 is contained on acting rotor shaft 6, rotor suction port 4 that described body 1 is calmed the anger communicates with centrifugal rotor 2 of calming the anger, described non-turbine-type acting rotor 3 is unshrouded impeller structures, described impeller upper blade 28 is fixed on wheel body not with the contact of chamber wall, described rotor shaft 5 of calming the anger is coaxial connections with acting rotor shaft 6, described calm the anger rotor shaft 5 and acting rotor shaft 6 are equipped with bearing 7 in body 1 spacing wall, throat less chamber is had in body 1 above described acting rotor 3 chamber, there is the cylindrical piston 8 matched with firing chamber inner circle described cylindrical combustion indoor, described cylindrical piston 8 periphery there is sealed piston ring 9, described cylindrical piston 8 is divided into front chamber 10 and rear chamber 11 firing chamber, cylindrical piston 8 can slide in the front chamber 10 of firing chamber and rear chamber 11, there is fumarole 12 at described piston 8 center, fumarole 12 center be equipped with can antero posterior axis to the fuel injector 13 of activity, described fumarole 12 there is guiding piece 27, spring 14 is had in described cylindrical piston 8 rear end firing chamber rear chamber 11, piston position controller 15 is had in described spring 14 rear end firing chamber rear chamber 11, telescopic pipe 16 is had in described spring 14 encloses, described telescopic pipe 16 front end is communicated with fuel injector 13, described telescopic pipe 16 rear end is through piston position controller 15, body 1 is communicated with fuel supplying device 17, described firing chamber rear chamber 11 rear end communicates with rotor air outlet 18 of calming the anger, described rotor air outlet 18 of calming the anger there is gas storage valve 19, described gas storage valve 19 communicates with the outer caisson 20 of body 1, described firing chamber front chamber 10 front end is communicated with acting rotor suction port 21, described firing chamber front chamber 10 front end acting rotor suction port 21 is provided with ignition mechanism 22 and flameholder 23, there is rotatable cam axle 24 at described acting rotor suction port 21 place, described acting rotor air outlet 25 communicates with air outlet flue 26.

Basic functional principle and advantage: gas storage valve 19 cuts out rotor air outlet 18 of calming the anger and opens caisson 20, the pressurized air with certain pressure enters in firing chamber rear chamber 11 through gas storage valve 19 and promotes piston 8 forward slip increasing fumarole 12 aperture, pressurized air spray into from fumarole 12 firing chamber front chamber 10 simultaneously fuel injector 13 spray fuel and be mixed to form inflammable mixture with pressurized air, an inflammable mixture part enters in flameholder 23 to be converged by ignition mechanism 22 ignition combustion expansion generation high-temperature high-pressure fuel gas through flameholder 23 with the inflammable mixture flow through outside flameholder 23, high-temperature high-pressure fuel gas promotes micro-camshaft 24 that the opens while that piston 8 reducing fumarole 12 aperture to rear chamber 11 sliding compression spring 14 and opens acting rotor 3 suction port 21, high-pressure gas sprays into through acting rotor 3 suction port 21 and promotes blade 28 in acting rotor 3 chamber acting rotor 3 is rotated in the counterclockwise direction, waste gas enters air outlet flue 26 through acting rotor 3 air outlet 25 and discharges, acting rotor 3 drives the rotor 2 of calming the anger coaxially to rotate, air enters in centrifugal rotor 2 of calming the anger through rotor 2 suction port 4 of calming the anger and form the pressurized air with certain pressure at air outlet 18 place after centrifugal rotor 2 of calming the anger pressurizes, gas storage valve 19 cuts out caisson 20 and opens rotor 2 air outlet 18 of calming the anger simultaneously, pressurized air enters in firing chamber rear chamber 11 through air outlet 18 and sprays in the firing chamber front chamber 10 of people's High Temperature High Pressure through fumarole 12, promote acting rotor 3 with high-temperature high-pressure fuel gas together burning expansion after the fuel mix sprayed with fuel injector 13 and rotate acting, acting rotor shaft 6 output power.When needing slow-speed of revolution low-power to export, telescopic pipe 16 extends and makes fuel injector 13 be moved along to foremost in fumarole 12, make fumarole 12 aperture minimum, under uniform pressure, jet amount is minimum, fuel injector 13 sprays into minimum fuel, in firing chamber front chamber 10, gaseous-pressure is lower, acting rotor 3 rotating speed is lower, because acting rotor 3 is non-turbine-type impellers, combustion gas breakage is compared with turbine-type impeller less during low speed, low-speed running is steady, when needs improve rotating speed increasing output power, telescopic pipe 16 retraction makes fuel injector 13 pressurized gas that mobile increasing fumarole 12 aperture sprays in firing chamber front chamber 10 backward in fumarole 12 increase, fuel injector 13 increasing fuel straying quatity simultaneously, in firing chamber front chamber 10, fuel gas temperature gaseous-pressure improves simultaneously, rotate clockwise the aperture that camshaft 24 strengthens suction port 21, the impetus power acted on acting rotor 3 blade 28 improves, acting rotor 3 outputting torsion strengthens rotating speed and improves, fumarole 12 variable makes firing chamber rear chamber 11 under identical operating air pressure, spray into the controlled of compressed air stream quantitative change in firing chamber front chamber 10, the pressurized gas straying quatity sprayed in firing chamber front chamber 10 can be changed when without the need to changing pressure, also have, the variable combustion of the inflammable mixture/gas that makes of two items of fuel straying quatity and pressurized gas straying quatity is than more easy to control, under identical working pressure increasing output power namely improve in outputting torsion and the process of rotating speed can make the combustion/gas of inflammable mixture than relative remain in optimum value constant, this can only the internal-combustion engine of individual event change not accomplished, the ubiquitous phenomenon of internal-combustion engine that existing individual event changes is---emit a burst of dense smoke during acceleration, have plenty of and reduce acceleration to improve this defect, also have, when the timing of fumarole 12 size one, under identical working pressure, jet amount is certain, its power range is just limited at maximum combustion/gas of inflammable mixture than following between minimum combustion/gas ratio, two items of fuel straying quatity and pressurized gas straying quatity are variable power stage scope is become wider, also have, in work when rotor 3 load that does work increases, its rotating speed reduces, amount of consumed gas reduces, in firing chamber front chamber 10, gaseous-pressure rising makes piston 8 slide toward rear chamber 11, reduce fumarole 12 aperture, reduce pressurized gas straying quatity, combustion/gas the ratio of inflammable mixture is improve under equal fuel straying quatity, the simultaneous temperature and the pressure that export gas quantity minimizing in firing chamber front chamber 10 raise, the active force acted on acting rotor 3 blade 28 raises, acting rotor 3 rotating speed raises, amount of consumed gas raises, in firing chamber front chamber 10, gaseous-pressure declines, piston 8 slides toward front chamber 10 under the pressure of spring 14 and pressurized gas, strengthen fumarole 12 aperture, strengthen pressurized gas straying quatity, combustion/gas the ratio of inflammable mixture is reduced under equal fuel straying quatity, in firing chamber front chamber 10, while temperature and pressure reduction, combustion gas output quantity increases, make it have very high adaptive ability, described telescopic pipe 16 makes fuel obtain good preheating in the process by telescopic pipe 16 in firing chamber rear chamber 11, advantage also has, can spring 14 be promoted by piston position controller 15 or pull the position of spring 14 pairs of pistons 8 to adjust, as: when use hydrogen, liquid gas, rock gas, during the gaseous fuels such as coal gas, due to the diffusivity of gaseous fuel, flammability is all relatively high, the front position that spring 14 to be pushed into piston 8 forward firing chamber front chamber 10 is promoted with piston position controller 15, make the capacity relative of firing chamber front chamber 10 less, the described piston 8 that makes is the shortest to the distance of acting rotor 3 suction port 21, when use gasoline, light kerosene, during the volatile liquid fuel such as alcohol, by the diffusivity of this class A fuel A, flammability is higher, available piston position controller 15 pull spring 14 piston 8 to be adjusted back in firing chamber before and after relative middle section position between chamber, when use kerosene, during the not volatile heavy class A fuel A such as diesel oil, spring 14 can be pulled piston 8 to be adjusted back in firing chamber in rear chamber 11 position rearward with piston position controller 15, make firing chamber front chamber 10 length relatively the longest, extend fuel from injection, be mixed into the distance of burning, relatively extend fuel to do time in advance with compressed-air actuated, pressurized air in firing chamber rear chamber 11 is when fumarole 12 sprays into firing chamber front chamber 10, spray in the shape of a spiral in firing chamber front chamber 10 by several angle under the guide functions of pressurized air guiding groove 27 in fumarole 12 and form eddy current, extend fuel relatively further from injection, be mixed into the distance of burning, extend fuel relatively further and improve mixture homogeneity diffusion time, make fuel combustion more abundant, it is wider that firing chamber variable adjustable controlled makes fuel Applicable scope become.

Fig. 4, Fig. 5 shows this programme second embodiment, can be found out by accompanying drawing, internal combustion engine shown in the present embodiment is equally by body 1, centrifugal calm the anger rotor 2 and non-turbine-type acting rotor 3 form, described rotor 2 of calming the anger same axis is arranged on respectively in body 1 rotor 2 chamber of calming the anger with acting rotor 3 in body 1, in acting rotor 3 chamber, described rotor 2 of calming the anger is contained in calms the anger on rotor shaft 5, described acting rotor 3 is contained on acting rotor shaft 6, comparing difference with the first embodiment is: acting rotor shaft 6 is connected through planetary gear set 32 with rotor shaft 5 of calming the anger, planetary gear set 32 has planetary gear set control gear 33.Because planetary gear set 32 is a kind of special gear structures, multiple connection mode can be had, now simply introduce single planetary gear set several connection modes the most basic in this programme, connection mode one: on the sun gear that can be connected in planetary gear set 32 with rotor shaft 5 of calming the anger, in the planetary carrier that acting rotor shaft 6 is connected in planetary gear set 32 in the heart, the gear ring in planetary gear set 32 is in free state, connection mode two: on the sun gear that also can be connected in planetary gear set 32 with rotor shaft 5 of calming the anger, acting rotor shaft 6 is connected in the gear ring disc centre in planetary gear set 32, and the planetary carrier in planetary gear set 32 is in free state, connection mode three: can also to be connected in the planetary carrier in planetary gear set 32 in the heart with rotor shaft 5 of calming the anger, described acting rotor shaft 6 is connected on the sun gear in planetary gear set 32, and the gear ring in planetary gear set 32 is in free state, connection mode four: can also be connected in the gear ring disc centre in planetary gear set 32 with rotor shaft 5 of calming the anger, acting rotor shaft 6 is connected on the sun gear in planetary gear set 32, and the planetary carrier in planetary gear set 32 is in free state, connection mode five: can also be connected in the gear ring disc centre in planetary gear set 32 with rotor shaft 5 of calming the anger, the sun gear in planetary gear set 32 is in free state in the planetary carrier that acting rotor shaft 6 is connected in planetary gear set 32 in the heart, connection mode six: on the planetary carrier that can also be connected in planetary gear set 32 with rotor shaft 5 of calming the anger, acting rotor shaft 6 is connected in the gear ring disc centre in planetary gear set 32, sun gear in planetary gear set 32 is in free state, in above six kinds of connection modes: when planetary gear set control gear 33 is wantonly two lockings in planetary gear set 32, acting rotor 3 is identical with the coaxial transmission of the first embodiment with rotating speed transmission with rotor 2 of calming the anger, when the resistance be in free state given in planetary gear set 32 by planetary gear set control gear 33, rotor 2 of calming the anger follows the rotating ratio of acting rotor 3 increase along with this resistance to be changed, when this resistance increases until infinity is namely in planetary gear set 32 during free term locking, rotor 2 of calming the anger compares transmission with acting rotor 3 by by the maximum of setting or minimum speed, difference also has: described acting rotor 3 chamber is oval, described acting rotor 3 is double shrouded wheel structures, described blade 28 both sides are by taking turns sheet 31 shutoff, described acting rotor 3 impeller upper blade 28 is arranged in wheel body axial notch 29, described axial notch 29 bottom blade 28 interior edge face there is spring 30, described acting rotor 3 chamber sidewall have with annular gas tank 34 corresponding bottom axial notch 29, vent 35 bottom axial notch 29 on wheel sheet 31 communicates with annular gas tank 34, described annular gas tank 34 communicates with acting rotor air outlet 25 through air flue 36, the oval part in described acting rotor 3 chamber follows blade 28 with wide, the thickness of its circular portion two wheel sheets 31 wider than blade 28, the advantage of double shrouded wheel is the sealing that improve acting rotor 3, make combustion gas side leakage less, combuster in body 1 above acting rotor 3 chamber, described firing chamber and other basic structure follow the first embodiment identical with working principle, in work, high-pressure gas in firing chamber front chamber 6 enters in acting rotor 3 chamber through suction port 21, promoting acting rotor 3 blade 28 makes acting rotor 3 rotate in the counterclockwise direction, blade 28 its end face under spring 30 thrust withstands on the inner headed face of oval acting rotor 3 chamber all the time, waste gas under pump-absorb action in air outlet 25 is through air flue 36, annular gas tank 34, vent 35 enters in bottom axial notch 29, described blade 28 to turn over after central vertical line in bottom axial notch 29 waste gas progressively through vent 35, described annular gas tank 34, air flue 36 is discharged in air outlet 25, the benefit of oval acting rotor chamber after blade 28 leaves acting rotor 3 suction port 21, is continued to promote blade 28 by the high-pressure gas that blade 28 seals by himself expansive force acting rotor 3 is rotated, efficiency gas is higher, shortcoming is that blade 28 end face is with the contact of acting rotor chamber inner headed face, produce certain surface friction drag, hot environment lower blade 28 weares and teares comparatively fast, the advantage of planetary gear set 32 is that the rotor 2 that makes to calm the anger can improve rotating speed and also can reduce rotating speed in the geostationary situation of acting rotor 3 rotating speed, the pressurized air of different compression ratio can be provided to firing chamber in the geostationary situation of acting rotor 3 rotating speed, realize the adjustable variable controllable of compression ratio.

Fig. 6, Fig. 7 shows this programme the 3rd embodiment, can be found out by accompanying drawing, internal combustion engine shown in the present embodiment is equally by body 1, centrifugal calm the anger rotor 2 and non-turbine-type acting rotor 3 form, described rotor 2 of calming the anger same axis is arranged on respectively in body 1 rotor 2 chamber of calming the anger with acting rotor 3 in body 1, in acting rotor 3 chamber, described rotor 2 of calming the anger is contained in calms the anger on rotor shaft 5, described acting rotor 3 is contained on acting rotor shaft 6, comparing difference with the first embodiment is: described acting rotor 3 is thin body double shrouded wheel structures, blade 28 is fixed on wheel body, blade 28 and wheel Zhou Kuandu are greater than wheel body width, blade both sides are by taking turns sheet 31 shutoff, advantage is the intensity and the sealing that improve blade, the weight of impeller is alleviated under same size, difference: described acting rotor 3 has with blade 28 with wide tongue piece 39 between adjacent two blades 28, a limit of described tongue piece 39 with blade 28 top margin in adjacent two blades 28 through the Viability connection of movable axis 40, described movable axis 40 is on the top margin of acting rotor 3 blade 28 clockwise blade face, tongue piece 39 is slide up and down in the scope between 0-90 degree of the blade face of its another edge, axle center another blade 28 adjacent with movable axis 40, its top dead center is no more than corresponding blade 28 top margin slided, the slip radian of 28 its radians of camber of the blade corresponding to described tongue piece 39 sliding edge and tongue piece 39 sliding edge matches, adjacent two blades 28 when tongue piece 39 active edges is at top dead center, the rotor cavity 41 of an opposing seal is formed between the wheel sheet 31 on tongue piece 39 and wheel week and blade 28 both sides, described acting rotor 3 chamber sidewall there is annular gas tank 34 corresponding with rotor cavity 41, described annular gas tank 34 communicates with acting rotor 3 air outlet 25 through air flue 36, communicate with corresponding annular gas tank 34 on the sidewall of acting rotor 3 chamber through vent 35 bottom described rotor cavity 41, there is gas exhausting valve 38 acting rotor 3 air outlet 25 with on the outer air outlet flue 26 in air flue 36 place of communicating of annular gas tank 34.Its working principle compares difference and advantage with the first embodiment: in the geostationary situation of gaseous-pressure provided in firing chamber front chamber 10 in work, high-pressure gas sprays in acting rotor 3 chamber through acting rotor 3 suction port 21, tongue piece 39 on acting rotor 3 blade 28 slides under the pressure of high-pressure gas in rotor cavity 41, high-pressure gas promotes blade 28 makes acting rotor 3 rotate in the counterclockwise direction, waste gas enters air outlet flue 29 through acting rotor 3 air outlet 25 and discharges, acting rotor shaft 18 output power, when the rotor 3 that does work needs low speed light running, adjustment camshaft 24 makes suction port 21 aperture less, the gaseous-pressure acted on acting rotor 3 blade 28 is relatively little, suitably turn gas exhausting valve 38 on air outlet flue 26 down and improve the exhaust gas pressure of acting rotor 3 air outlet 25, in adjustment air flue 26, air valve 37 makes waste gas only enter not toward going out in annular gas tank 34, exhaust gas pressure in acting rotor 3 upper rotor part cavity 41 is improved relatively, tongue piece 39 on acting rotor 3 blade 28 is upwards in relatively high position toward outer slip of rotor cavity 41 under the exhaust gas pressure effect relatively improved, make acting rotor 3 week/air displacement is relatively low, rotor 3 outputting torsion that now does work is compared little.When the rotor 3 that does work needs low speed high-load operation, suitable increasing camshaft 24 aperture, act on the gaseous-pressure enlarged relative on acting rotor 3 blade 28, suitably tune up gas exhausting valve 38 aperture on air outlet flue 26 and reduce acting rotor 3 air outlet 25 pressure, in adjustment air flue 26, air valve 37 makes waste gas only export but no import in annular gas tank 34, rotor cavity 41 internal pressure on acting rotor 3 is reduced relatively, act on exhaust gas pressure reduction upwards below tongue piece 39, tongue piece 39 on described acting rotor 3 blade 28 slides into lower dead center downwards under the effect of high-pressure gas pressure in rotor cavity 41, now do work rotor 3 week/air displacement is relatively maximum, outputting torsion is compared maximum.When the rotor 3 that does work needs high speed high-load operation, continue to strengthen camshaft 24 aperture until maximum, the gaseous-pressure acted on acting rotor 3 blade 28 is maximum, gas exhausting valve 38 standard-sized sheet on air outlet flue 26, in same adjustment air flue 26, air valve 37 makes waste gas only export but no import in annular gas tank 34, make exhaust gas pressure in the rotor cavity 41 on acting rotor 3 relatively minimum, act on tongue piece 39 to upward pressure below reduction, acting rotor 3 rotating speed improves relatively, act on that centrifugal force on tongue piece 39 is higher to be made tongue piece 39 lower dead center left in rotor cavity 41 slide outward to be in relatively low position, now do work rotor 3 week/air displacement is relatively large, it is relatively maximum that outputting torsion compares reduction output power.When the rotor 3 that does work needs high speed light running, suitably turn gas exhausting valve 38 aperture on air outlet flue 26 down and improve acting rotor 3 air outlet 25 pressure, in adjustment air flue 26, air valve 37 makes waste gas only import but no export in annular gas tank 34, rotor cavity 41 internal pressure on acting rotor 3 is improved relatively, tongue piece 39 below exhaust gas pressure upwards raises and adds that the centrifugal force acted on tongue piece 39 is stronger, tongue piece 39 upward sliding is high position extremely relatively, the aperture suitably turning camshaft 24 down improves gas flow rate, now do work rotor 3 week/the relatively little rotating speed of air displacement is higher, outputting torsion is compared little, different also have: described acting rotor shaft 6 connects through planetary gear set 32 with rotor shaft 5 of calming the anger, described planetary gear set 32 there is planetary gear set control gear 33, the advantage of planetary gear set 32 and planetary gear set control gear 33 describes in a second embodiment, here no longer carefully state, above-mentioned workflow will accomplish that under the cooperation completely of firing chamber and planetary gear set 32 and planetary gear set control gear 33 the large torsion of the large air displacement of the slow-speed of revolution exports completely, the low torsion of the low air displacement of high rotating speed exports, the little torsion of the low air displacement of low speed exports, the high-power output of the high air displacement of high speed.

Fig. 8, Fig. 9, Figure 10 collectively illustrates this programme the 4th embodiment, can be found out by accompanying drawing, internal combustion engine shown in the present embodiment is equally by body 1, centrifugal calm the anger rotor 2 and non-turbine-type acting rotor 3 form, described acting rotor 3 chamber is equally oval with rotor 3 chamber of doing work in the second embodiment, described rotor 2 of calming the anger same axis is arranged on respectively in body 1 rotor 2 chamber of calming the anger with acting rotor 3 in body 1, in acting rotor 3 chamber, described rotor 2 of calming the anger is contained in calms the anger on rotor shaft 5, described acting rotor 3 is contained on acting rotor shaft 6, described blade 28 is same in wheel body axial notch 29, spring 30 is had in described blade 28 lower end surface axial notch 29, described rotor shaft 5 of calming the anger is connect by planetary gear set 32 with acting rotor shaft 6 equally, planetary gear set 32 there is planetary gear set control gear 33, difference is: described acting rotor 3 is unshrouded impeller structures, described impeller there is tongue piece 39 between adjacent two blades 28, described tongue piece 39 is gone here and there by tongue piece convex body 45 and tongue piece concave volume 44 to insert the Collapsible structure that forms, described tongue piece concave volume 44 internal tongue convex body 45 top end there is tongue piece spring 46, described blade 28 top end there is vane groove 42, have in described vane groove 42 and contact with oval acting rotor 3 chamber inner headed face with wide roller 43 with blade 28, advantage becomes rolling friction from direct friction to reduce wearing and tearing and reduce resistance, a limit of described tongue piece convex body 45 with blade 28 top margin in adjacent two blades 28 through the Viability connection of movable axis 40, described movable axis 40 is on the top margin of acting rotor 3 blade 28 counterclockwise blade face, described tongue piece 39 is that the exterior rim of its tongue piece concave volume 44 of axle center slides up and down along in scope between 0-90 degree of the blade face of another blade 28 adjacent with movable axis 40, its top dead center is no more than corresponding blade 28 top margin slided, the slip radian of 28 its radians of camber of the blade corresponding to described tongue piece 39 sliding edge and tongue piece 39 matches, described tongue piece concave volume 44 its exterior rim under the active force of spring 46 follows corresponding 28, blade contact of sliding all the time, described tongue piece concave volume 44 exterior rim is adjacent two blades 28 when top dead center, the tongue piece 39 that tongue piece concave volume 44 is formed with tongue piece convex body 45, the rotor cavity 41 of an opposing seal is formed between wheel body and acting rotor 3 liang of chamber walls, spring 30 is had in rotor cavity 41 below described tongue piece 39, described acting rotor 3 chamber sidewall there is annular gas tank 34 with corresponding bottom axial notch 29, described annular gas tank 34 communicates with acting rotor 3 air outlet 25 through air flue 36, communicate with corresponding annular gas tank 34 on the sidewall of acting rotor 3 chamber bottom axial notch 29, there is gas exhausting valve 38 acting rotor 3 air outlet 25 with on the outer air outlet flue 26 in air flue 36 place of communicating of annular gas tank 34, its upper end of vane hole 47 is had to communicate with bottom axial notch 29 with the lower end that communicates bottom rotor cavity 41 in described blade 28, the difference comparing basic functional principle with the 3rd embodiment with second is: described tongue piece 39 its tongue piece concave volume 44 exterior rim under the active force of spring 30 is in corresponding blade 28 top edge of sliding, blade 28 makes roller 43 in its end face groove 42 contact with oval acting rotor 3 inner headed face by active force outside slip in axial notch 29 of spring 30 bottom tongue piece 39 lower spring 30 and axial notch 29, high-pressure gas in described firing chamber front chamber 10 enters in acting rotor 3 chamber through camshaft 24 and suction port 21, first high-pressure gas makes tongue piece 39 along the downslide of 28, blade, promoting blade 28 makes acting rotor 3 rotate in the counterclockwise direction, in described blade 28 end face groove 42, roller 43 rolls along the inner headed face in ellipse acting rotor 3 chamber, described blade 28 along with ellipse acting face, rotor 3 chamber outwards skid off in axial notch 29, described blade 28 to turn in oval acting rotor 3 chamber after the large nose circle of longest diameter line along with ellipse acting rotor 3 chamber inner headed face slides in axial notch 29, tongue piece concave volume 44 exterior rim of described tongue piece 39 withstands on corresponding 28, the blade slided all the time under the active force of spring 46, the present position of tongue piece concave volume 44 exterior rim on 28, the blade of corresponding slip of described tongue piece 39 is subject to toward exhaust gas pressure in interior gaseous-pressure and rotor cavity outward 41, spring 30 active force, and the interaction of centrifugal force controls, can by exhaust gas pressure in the gas exhausting valve 38 corresponding regulation and control rotor cavity 41 in air valve 37 in air flue 36 and air outlet flue 26 and then the present position of tongue piece concave volume 44 exterior rim on 28, the blade of corresponding slip controlling tongue piece 39 in work, realize to acting rotor 3 week/control of air displacement, specific works process no longer describes here with describing in the 3rd embodiment.

Figure 11, Figure 12, Figure 13 collectively illustrates this programme the 5th embodiment, can be found out by accompanying drawing, internal combustion engine shown in the present embodiment is by body 1, centrifugal rotor 2 and the non-turbine-type acting rotor formation of calming the anger, described non-turbine-type acting rotor is made up of do work rotor 3 and the second acting rotor 3 ', described acting rotor 3 and the second acting rotor 3 ' are all double shrouded wheel structures, described rotor 2 of calming the anger, acting rotor 3 and the second acting rotor 3 ' same axis are arranged on respectively in body 1 rotor 2 chamber of calming the anger in body 1, acting rotor 3 chamber and second is done work in rotor 3 ' chamber, described rotor 2 of calming the anger is contained in calms the anger on rotor shaft 5, described acting rotor 3 is contained on acting rotor shaft 6, described second acting rotor 3 ' is contained on acting rotor shaft 6 ', described acting rotor shaft 6 does not connect with the second acting rotor shaft 6 ', acting rotor shaft 6 has bearing 7 with on the second acting rotor shaft 6 ', described acting rotor shaft connects with rotor shaft 5 of calming the anger through planetary gear set 32, described planetary gear set 32 there is planetary gear set control gear 33, described acting rotor 3 and the second acting rotor 3 ' share a firing chamber on acting rotor 3 chamber and the second acting rotor 3 ' chamber in body 1, described firing chamber is identical with the firing chamber described in the first embodiment, described rotor 2 air outlet 18 of calming the anger is communicated with firing chamber rear chamber 11 rear end, described air outlet 18 there is gas storage valve 19, described gas storage valve 19 is communicated with the outer caisson 20 of body 1, described firing chamber front chamber 10 front end is communicated with the second acting rotor 3 ' with acting rotor 3 with the second acting rotor suction port 21 ' through acting rotor suction port 21 respectively, described acting rotor suction port 21 and the second acting rotor suction port 21 ' are equipped with camshaft 24 respectively, described acting rotor 3 is the same with the second acting rotor 3 ' structure with rotor 3 difference of doing work in the 3rd embodiment is: described acting rotor 3 and the second acting rotor 3 ' are that wheel body follows blade 28 with wide double shrouded wheel structure, annular gas tank 34 on described second acting rotor 3 ' chamber sidewall follows the annular gas tank 34 done work on the sidewall of rotor 3 chamber respectively on relative chamber, both sides wall, annular gas tank 34 on the sidewall of described acting rotor 3 chamber communicates with acting rotor air outlet 25 through air flue 36, annular gas tank 34 on second acting rotor 3 ' chamber sidewall communicates with the second acting rotor air outlet 25 ' through the second air flue 36 ', described acting rotor 3 is connected movable axis 40 on the top margin of blade counterclockwise lateral lobe face with the tongue piece 39 on the second acting rotor 3 ', described acting rotor air outlet 25 is communicated with air outlet flue 26 jointly with the second acting rotor air outlet 25 ', share a gas exhausting valve 38, embodiment is identical for other structure all with three.Basic functional principle: described gas storage valve 19 cuts out rotor 2 air outlet 18 of calming the anger and opens caisson 20, the pressurized air in described caisson 20 with certain pressure enters in firing chamber rear chamber 11 through gas storage valve 19 and promotes piston 8 to front chamber 10 slip increasing fumarole 12 aperture, pressurized air sprays into firing chamber front chamber 10 from fumarole 12, simultaneously fuel injector 13 sprays fuel and is mixed to form inflammable mixture with pressurized air, an inflammable mixture part enters in flameholder 23 to converge with the inflammable mixture that another part does not enter flameholder 23 through flameholder 23 and is lighted expanding combustion by igniter 22 and generate high-pressure gas, high-temperature high-pressure fuel gas promotes micro-camshaft 24 opened on acting rotor suction port 21 and the second acting rotor suction port 21 ' while that piston 8 reducing fumarole 12 aperture to rear chamber 11 sliding compression spring 14 and opens acting rotor suction port 21 and the second acting rotor suction port 21 ', high-pressure gas sprays to acting rotor 3 and the second acting rotor 3 ' through acting rotor suction port 21 and the second acting rotor suction port 21 ', described acting rotor 3 and the second tongue piece 39 done work on rotor 3 ' blade 28 slide downward under the pressure of high-pressure gas promotes, the resistance that described second acting rotor shaft 6 ' acts on more greatly on the second acting rotor 3 ' for power stage thrust load is just larger, the resistance compared on acting rotor 3 is less, first high-pressure gas promotes acting rotor 3 and rotates, acting rotor 3 drives rotor 2 of calming the anger to rotate through planetary gear set 32, air enters in centrifugal rotor 2 of calming the anger through rotor suction port 4 of calming the anger and form the pressurized air with certain pressure in air outlet 18 after centrifugal rotor 2 of calming the anger pressurizes, described gas storage valve 19 cuts out caisson 20 and opens rotor air outlet 18 of calming the anger simultaneously, pressurized air enters the fuel mix sprayed with fuel injector 13 through fumarole 12 Pen Ren firing chamber front chamber 10 in firing chamber rear chamber 11 and becomes inflammable mixture through air outlet 18, inflammable mixture improves acting rotor 3 rotating speed further with high-temperature high-pressure fuel gas in firing chamber front chamber 10 together burning expansion, when in firing chamber front chamber 10, gaseous-pressure is brought up to a certain degree, the high-pressure gas active force acted on the second acting rotor 3 ' resistance overcome on the second acting rotor 3 ' promotes the second acting rotor 3 ' and rotates, second acting rotor shaft 6 ' end output power.Relevant planetary gear set 32 and planetary gear set control gear 33 describe in detail in a second embodiment, here no longer repeated description, the present embodiment advantage: owing to there being two rotors that do work, in work, when the load of the second acting rotor 3 ' increases, its rotating speed reduces the corresponding reduction of air displacement, the corresponding raising of gaseous-pressure in firing chamber front chamber 10, the gaseous-pressure of respective action on acting rotor 3 improves, the corresponding raising of rotating speed of described acting rotor 3, the rotating speed also corresponding raising of the rotor 2 of calming the anger that acting rotor 3 drives, the pressurized gas flow raising all corresponding to pressurized gas pressure that rotor 2 of calming the anger provides to firing chamber rear chamber 11, in firing chamber front chamber 10, gaseous-pressure is also thereupon corresponding is improved, act on the gaseous-pressure also corresponding raising on the second acting rotor 3 ', the rotating speed just corresponding raising of the second acting rotor 3 ', its rotating speed raising corresponding to air displacement when the load of the second acting rotor 3 ' reduces, the corresponding reduction of gaseous-pressure in firing chamber front chamber 10, the gaseous-pressure of respective action on acting rotor 3 also reduces, the rotating speed also corresponding reduction of acting rotor 3, by the rotating speed also corresponding reduction of the rotor 2 of calming the anger that acting rotor 3 drives, rotor 2 of calming the anger is supplied to the pressurized gas flow reduction all corresponding to pressurized gas pressure of firing chamber rear chamber 11, gaseous-pressure also corresponding reduction thereupon in described front chamber 10, act on the gaseous-pressure equally also corresponding reduction on the second acting rotor 3 ', the corresponding reduction of rotating speed of the second acting rotor 3 ', when the load of the second acting rotor 3 ' increase to infinitely great namely the second acting rotor 3 ' stops operating time, acting rotor 3 can also keep alone running.Press down air rotor at various complex working conditions automatically to adjust according to the change of payload with acting rotor, acting rotor accomplishes self adaption with calming the anger between rotor, clutch can be saved in power stage process, optimum Match can be accomplished with automatic transmission case, make loss in power transimission process less, operate simpler.

Figure 14, Figure 15, Figure 16 collectively illustrates this programme the 6th specific embodiment, can be found out by accompanying drawing, internal combustion engine shown in the present embodiment is by body 1, centrifugal rotor 2 and the non-turbine-type acting rotor formation of calming the anger, described acting rotor is by the rotor 3 that does work, the rotor of the second acting rotor 3 ' and the 3rd acting rotor 3 〞 tri-unshrouded impeller structures is formed, described rotor 2 of calming the anger, acting rotor 3 and the second acting rotor 3 ' and the 3rd acting rotor 3 〞 same axis are arranged on respectively in body 1 rotor 2 chamber of calming the anger in body 1, acting rotor 3 chamber, second acting rotor 3 ' chamber and the 3rd is done work in rotor 3 〞 chamber, described rotor 2 of calming the anger is contained in calms the anger on rotor shaft 5, described acting rotor 3 is contained on acting rotor shaft 6, described second acting rotor 3 ' is contained on acting rotor shaft 6 ', described 3rd acting rotor 3 〞 is contained on the 3rd acting rotor shaft 6 〞, described rotor shaft 5 of calming the anger is coaxial connections with acting rotor shaft 6, described acting rotor shaft 6 connects with the second acting rotor shaft 6 ' planetary gear set 32, described second acting rotor shaft 6 ' connects by planetary gear set 32 with the 3rd acting rotor shaft 6 〞, described planetary gear set 32 there is planetary gear set control gear 33, described 3rd acting rotor shaft 6 〞 end is power take-off, the independent air outlet flue 26 in the independent firing chamber of described acting rotor 3, described second acting rotor 3 ' and the 3rd acting rotor 3 〞 share one, the second firing chamber second row air flue 26 ', described rotor air outlet 18 of calming the anger communicates with firing chamber rear chamber 11 and the second firing chamber rear chamber 11 ', there is air valve 37 described rotor air outlet 18 of calming the anger with after firing chamber rear chamber 11 between the second firing chamber rear chamber 11 ', described acting rotor suction port 21 communicates with firing chamber front chamber 10 front end, second acting rotor suction port 21 ' is communicated with in the second firing chamber front chamber 10 ' front end with described 3rd acting rotor suction port 21 〞 jointly, described acting rotor suction port 21, second acting rotor suction port 16 ' and the 3rd acting rotor suction port 16 〞 there is camshaft 24, described acting rotor 3 has with blade 28 with wide tongue piece 39 between adjacent two blades 28, a limit of described tongue piece 39 with blade 28 top margin in adjacent two blades 28 through the Viability connection of movable axis 40, described movable axis 40 is on the top margin of acting rotor 3 blade 28 counterclockwise blade face, described tongue piece 39 is slide up and down in the scope between 0-90 degree of the blade face of its another edge, axle center another blade 28 adjacent with movable axis 40, its top dead center is no more than corresponding blade 28 top margin slided, the slip radian of 28 its radians of camber of the blade corresponding to described tongue piece 39 sliding edge and tongue piece 39 sliding edge matches, adjacent two blades 28 when tongue piece 39 active edges is at top dead center, the rotor cavity 41 of an opposing seal is formed between the wheel sheet 31 on tongue piece 39 and wheel week and blade 28 both sides, acting rotor 3 chamber sidewall there is annular gas tank 34 corresponding with rotor cavity 41, described annular gas tank 34 communicates with acting rotor 3 air outlet 25 through air flue 36, communicate with corresponding annular gas tank 34 on the sidewall of acting rotor 3 chamber through vent 35 bottom rotor cavity 41, there is gas exhausting valve 38 acting rotor 3 air outlet 25 with on the outer air outlet flue 26 in air flue 36 place of communicating of annular gas tank 34, described second acting rotor 3 ' and the 3rd acting rotor 3 〞 chamber sidewall also there is annular gas tank 34 corresponding with the rotor cavity 41 on the second acting rotor 3 ' and the 3rd acting rotor 3 〞, second acting rotor 3 ' chamber is communicated with the 3rd acting rotor air outlet 25 〞 with the second acting rotor air outlet 25 ' with the 3rd air flue 36 〞 through the second air flue 36 ' respectively with the annular gas tank 34 on the 3rd acting rotor 3 〞 chamber sidewall, described air flue 36, second air flue 36 ' and the 3rd air flue 36 〞 there is air valve 37, second acting rotor air outlet 25 ' is communicated with on second row air flue 26 ' with the 3rd acting rotor air outlet 25 〞 jointly, described second row air flue 26 ' there is gas exhausting valve 38, described second acting rotor 3 ' is all identical with acting rotor 3 with other basic structure of the 3rd acting rotor 3 〞, described firing chamber and the basic structure of the second firing chamber all follow the firing chamber described in the first embodiment identical, described planetary gear set 32 is identical with planetary gear set control gear 33 with the planetary gear set 32 described in the second embodiment with planetary gear set control gear 33, be not repeated.Working principle: described gas storage valve 19 cuts out rotor air outlet 18 of calming the anger and opens caisson 20, the pressurized air in caisson 20 with certain pressure enters in firing chamber rear chamber 11 and the second firing chamber rear chamber 11 ' through gas storage valve 19, the pressurized air with certain pressure sprays into through fumarole 12 fuel mix sprayed with fuel injector 13 in firing chamber front chamber 10 and the second firing chamber front chamber 10 ' and forms inflammable mixture, inflammable mixture is generated high-temperature high-pressure fuel gas by ignition mechanism 22 ignition combustion, micro-camshaft 24 opened on each suction port opens acting rotor suction port 21 simultaneously, second acting rotor suction port 21 ' and the 3rd acting rotor suction port 21 〞, high-temperature high-pressure fuel gas is through acting rotor suction port 21, second acting rotor suction port 21 ' and the 3rd acting rotor suction port 21 〞 spray to acting rotor 3, second acting rotor 3 ' and the 3rd acting rotor 3 〞, acting rotor 3 and second tongue piece 39 slide downward under the pressure of high-pressure gas promotes of doing work on rotor 3 ' and the 3rd acting rotor 3 〞, high-pressure gas promotes the epitrochanterian blade 19 of each acting makes acting rotor 3 and the second acting rotor 3 ' and the 3rd acting rotor 3 〞 rotate acting, described acting rotor 3 drives rotor 2 of calming the anger to rotate through planetary gear set 32, air enters through rotor suction port 4 of calming the anger centrifugally calms the anger in rotor 2, the pressurized air with certain pressure is formed in air outlet 18 after centrifugal rotor 2 of calming the anger pressurizes, gas storage valve 19 cuts out caisson 20 and opens rotor air outlet 18 of calming the anger, the pressurized air that rotor air outlet 18 place has a certain pressure of calming the anger enters in firing chamber rear chamber 11 and the second firing chamber rear chamber 11 ' through air outlet 18, the fuel mix burning that the pressurized air with certain pressure sprays with fuel injector 11 from fumarole 12 Pen Ren firing chamber front chamber 10 and the second firing chamber front chamber 10 ' promotes acting rotor 3 and the second acting rotor 3 ' and the 3rd acting rotor 3 〞 and rotates acting.First can also start a firing chamber and enable other firing chamber, as: as described in gas storage valve 19 close rotor air outlet 18 of calming the anger and open caisson 20, close gas check valve 37 simultaneously and remove acting rotor shaft 6 with in planetary gear set control gear 33 pairs of planetary gear set 32 between the second acting rotor shaft 6 ' wantonly two locking and make free term be in free state to the control of free term in planetary gear set 32, the pressurized air in caisson 20 with certain pressure enters in firing chamber rear chamber 11 through gas storage valve 19, the pressurized air with certain pressure sprays into through fumarole 12 fuel mix sprayed with fuel injector 13 in front chamber 10 and forms inflammable mixture, inflammable mixture is generated high-temperature high-pressure fuel gas by ignition mechanism 22 ignition combustion, micro-camshaft 24 opened on suction port opens acting rotor suction port 21 simultaneously, high-temperature high-pressure fuel gas sprays to acting rotor 3 through acting rotor suction port 21, tongue piece 39 on acting rotor 3 is slide downward under the pressure of high-pressure gas promotes, the high-temperature high-pressure fuel gas blade 19 promoted on acting rotor 3 makes acting rotor 3 rotate acting, described acting rotor 3 drives rotor 2 of calming the anger to rotate through planetary gear set 32, air enters through rotor suction port 4 of calming the anger centrifugally calms the anger in rotor 2, the pressurized air with certain pressure is formed in air outlet 18 after centrifugal rotor 2 of calming the anger pressurizes, described gas storage valve 19 cuts out caisson 20 and opens rotor air outlet 18 of calming the anger, open air valve 37 simultaneously, the pressurized air that described rotor air outlet 18 place of calming the anger has certain pressure enters in firing chamber rear chamber 11 and the second firing chamber rear chamber 11 ' through air outlet 18, the fuel mix burning that the pressurized air with certain pressure sprays with fuel injector 11 from fumarole 12 Pen Ren firing chamber front chamber 10 and the second firing chamber front chamber 10 ' promotes acting rotor 3 and the second acting rotor 3 ' and the 3rd acting rotor 3 〞 and rotates acting.Advantage: owing to have employed two firing chambers at the present embodiment, three acting rotors, and all connected by planetary gear set 32 between three acting rotors, through planetary gear set control gear 33 can to regulate and control arbitrarily between each acting rotor and and the rotating ratio of calming the anger between rotor 2, regulate and control more flexible, air valve 37 can also be set calming the anger between rotor air outlet 18 and firing chamber rear chamber 11, closedown arbitrarily or any one of opening in two firing chambers can be needed can to make to only have one to work in three rotors that do work according to different power stages in work and also can make in three rotors that do work, to only have two work that three acting rotors can also be made all to work, its power stage accommodation is broader.

Figure 17, Figure 18 shows this programme the 7th specific embodiment, can be found out by accompanying drawing, internal combustion engine shown in the present embodiment is by body 1, centrifugal rotor 2 and the non-turbine-type acting rotor formation of calming the anger, described acting rotor is made up of do work rotor 3 and the second acting rotor 3 ', described rotor 2 of calming the anger, acting rotor 3 and the second acting rotor 3 ' same axis are arranged on respectively in body 1 rotor 2 chamber of calming the anger in body 1, acting rotor 3 chamber and second is done work in rotor 3 ' chamber, described rotor 2 of calming the anger is contained in calms the anger on rotor shaft 5, described second acting rotor 3 ' is contained on acting rotor shaft 6 ', described acting rotor 3 and the second acting rotor 3 ' share a firing chamber on acting rotor 3 chamber and the second acting rotor 3 ' chamber in body 1, described firing chamber is identical with the firing chamber described in the first embodiment, described rotor 2 air outlet 18 of calming the anger is communicated with firing chamber rear chamber 11 rear end, described air outlet 18 there is gas storage valve 19, described gas storage valve 19 is communicated with the outer caisson 20 of body 1, described firing chamber front chamber 10 front end is communicated with the second acting rotor 3 ' with acting rotor 3 with the second acting rotor suction port 21 ' through acting rotor suction port 21 respectively, described acting rotor suction port 21 and the second acting rotor suction port 21 ' are equipped with camshaft 24 respectively, described rotor shaft 5 of calming the anger connects with the second acting rotor shaft 6 ' through planetary gear set 32, described planetary gear set 32 there is planetary gear set control gear 33, described planetary gear set 32 and planetary gear set control gear 33 are all arranged in acting rotor 3 wheel body, described acting rotor 3 wheel body can be connected directly between on the bull gear 48 in planetary gear set 32, also the bull gear 48 in planetary gear set 32 can directly be substituted, can also directly connect with planetary carrier 49 center in planetary gear set 32, save acting rotor shaft 6, make overall structure compacter, volume is less, described second acting rotor shaft 6 ' directly connects with rotor shaft 5 of calming the anger through planetary gear set 32, Placement one: when acting rotor 3 wheel body substitutes the bull gear 48 in planetary gear set 32, second acting rotor shaft 6 ' and rotor shaft 5 of calming the anger can be connected in planetary carrier 49 center in planetary gear set 32 and sun gear 50 in the heart, Placement two: when acting rotor 3 wheel body to be connected in the planetary carrier 49 in planetary gear set 32 in the heart, second acting rotor shaft 6 ' and rotor shaft 5 of calming the anger can be connected in bull gear 48 in planetary gear set 32 and sun gear 50 in the heart, at work, when doing work rotor 3 locking, described second acting rotor 3 ' pacifies with rotor 2 of calming the anger the planetary gear set 32 rotating ratio transmission preset, when the rotor 3 that does work operates, rotation speed change with acting rotor 3 changes with the rotating ratio of calming the anger between rotor 2 by described second acting rotor 3 ', other operation mode describes in detail in a second embodiment, described rotor 2 of calming the anger, acting rotor 3, the basic structure of the second acting rotor 3 ' and firing chamber and working principle thereof are all identical with what describe in the 4th embodiment, be not repeated.

Figure 19, Figure 20 shows this programme the 8th specific embodiment, can be found out by accompanying drawing, internal combustion engine shown in the present embodiment to be calmed the anger rotor 52 by previous stage blade pump type, blade pump type calm the anger rotor 51 and non-turbine-type acting rotor 3 and body 1 form, described blade pump type rotor 51 and previous stage blade pump type rotor 52 of calming the anger of calming the anger is arranged on calm the anger rotor 51 chamber and previous stage blade pump type of blade pump type oval in body 1 respectively and calms the anger in rotor 52 chamber, described acting rotor 3 is arranged in body 1 inner cylindrical acting rotor 3 chamber, calm the anger rotor 51 and previous stage blade pump type of described blade pump type calms the anger rotor 52 and acting rotor 3 all in body 1 on the same axis line, described blade pump type rotor 51 of calming the anger is arranged on and calms the anger on rotor shaft 5 for final stage rotor of calming the anger, described previous stage blade pump type rotor 52 of calming the anger is arranged on previous stage and calms the anger on rotor shaft 55, described acting rotor 3 is arranged on acting rotor shaft 6, described calm the anger rotor shaft 5 and previous stage rotor shaft 55 of calming the anger is coaxial connections with acting rotor shaft 6, described body 1 has above the previous stage rotor 52 of calming the anger of one-level blade pump type in front of rotor suction port 53 of calming the anger to communicate, described previous stage rotor air outlet 54 of calming the anger is communicated with rotor suction port 4 of calming the anger, described suction port 4 is communicated with blade pump type rotor 51 of calming the anger, described rotor air outlet 18 of calming the anger there is gas storage valve 19, described gas storage valve 19 is communicated with the outer caisson 20 of body 1, described acting rotor 3 is unshrouded impeller structures, described impeller upper blade 28 is fixed on wheel body not with the contact of chamber wall, described previous stage is calmed the anger rotor shaft 55, calm the anger on rotor shaft 5 and acting rotor shaft 6 and bearing 7 is housed in body 1 spacing wall, throat less chamber is had in body 1 above described acting rotor 3 chamber, there is the cylindrical piston 8 matched with firing chamber inner circle described cylindrical combustion indoor, described cylindrical piston 8 periphery there is sealed piston ring 9, described cylindrical piston 8 is divided into firing chamber front chamber 10 and firing chamber rear chamber 11 firing chamber, described cylindrical piston 8 can slide in firing chamber front chamber 10 and firing chamber rear chamber 11, there is fumarole 12 at described piston 8 center, described fumarole 12 center be equipped with can antero posterior axis to the fuel injector 13 of activity, described fumarole 12 there is guiding piece 27, spring 14 is had in described cylindrical piston 8 rear end firing chamber rear chamber 11, piston position controller 15 is had in described spring 14 rear end firing chamber rear chamber 11, telescopic pipe 16 is had in described spring 14 encloses, described telescopic pipe 16 front end is communicated with fuel injector 13, rear end is through piston position controller 15, body 1 is communicated with fuel supplying device 17, described firing chamber rear chamber 11 rear end communicates with rotor air outlet 18 of calming the anger, described firing chamber front chamber 10 front end is communicated with acting rotor 3 suction port 21, described firing chamber front chamber 10 front end acting rotor 3 suction port 21 is provided with ignition mechanism 22 and flameholder 23, there is rotatable cam axle 24 at described acting rotor 3 suction port 21 place, described acting rotor 3 air outlet 25 communicates with air outlet flue 26, described acting rotor 3 impeller has with blade 28 with wide tongue piece 39 between adjacent two blades 28, a limit of described tongue piece 39 with blade 28 top margin in adjacent two blades 28 through the Viability connection of movable axis 40, described movable axis 40 is on the top margin of acting rotor 3 blade 28 counterclockwise blade face, described tongue piece 39 is slide up and down in the scope between 0-90 degree of the blade face of its another edge, axle center another blade 28 adjacent with movable axis 40, its top dead center is no more than corresponding blade 28 top margin slided, the slip radian of 28 its radians of camber of the blade corresponding to described tongue piece 39 sliding edge and tongue piece 39 sliding edge matches, adjacent two blades 28 when tongue piece 39 active edges is at top dead center, the rotor cavity 41 of an opposing seal is formed between the wheel sheet 31 on tongue piece 39 and wheel week and blade 28 both sides, described acting rotor 3 chamber sidewall there is annular gas tank 34 corresponding with rotor cavity 41, described annular gas tank 34 communicates with acting rotor air outlet 25 through air flue 36, described air flue 36 there is air valve 37, communicate with corresponding annular gas tank 34 on the sidewall of acting rotor 3 chamber bottom rotor cavity 41, there is gas exhausting valve 38 described acting rotor air outlet 25 with on the outer air outlet flue 26 in air flue 36 place of communicating of annular gas tank 34.Basic functional principle: described gas storage valve 19 cuts out rotor air outlet 18 of calming the anger and opens caisson 20, the pressurized air in described caisson 20 with certain pressure enters in firing chamber rear chamber 11 through gas storage valve 19 and promotes piston 8 to front chamber 10 slip increasing fumarole 12 aperture, pressurized air sprays into firing chamber front chamber 10 from fumarole 12, simultaneously fuel injector 13 sprays fuel and is mixed to form inflammable mixture with pressurized air, an inflammable mixture part enters in flameholder 23 to converge with the inflammable mixture that another part does not enter flameholder 23 through flameholder 23 and is lighted expanding combustion by igniter 22 and generate high-temperature high-pressure fuel gas, high-temperature high-pressure fuel gas promotes micro-camshaft 24 opened on acting rotor suction port 21 while that piston 8 reducing fumarole 12 aperture to rear chamber 11 sliding compression spring 14 and opens acting rotor suction port 21, high-pressure gas sprays to acting rotor 3 through acting rotor suction port 21, tongue piece 39 on described acting rotor 3 blade 28 slides under the pressure of high-pressure gas promotes in rotor cavity 41, high-pressure gas promotes blade 28 makes acting rotor 3 rotate, acting rotor 3 drives calm the anger rotor shaft 5 and previous stage rotor shaft 55 of calming the anger that blade pump type rotor 51 and previous stage blade pump type rotor 52 of calming the anger of calming the anger is rotated through acting rotor shaft 6, air enters previous stage blade pump type and calms the anger to calm the anger through previous stage vane pump formula in rotor 52 through previous stage rotor suction port 53 of calming the anger and to form the pressurized air with certain pressure after rotor 52 pressurizes and directly enter blade pump type and calm the anger in rotor 51 through calm the anger rotor air outlet 54 and rotor suction port 4 of calming the anger of previous stage and again compress through blade pump type rotor 51 of calming the anger the pressurized air that formation of pressurizeing has elevated pressures, described gas storage valve 19 cuts out caisson 20 and opens rotor air outlet 18 of calming the anger simultaneously, the pressurized air with elevated pressures enters the fuel mix sprayed with fuel injector 13 through fumarole 12 Pen Ren firing chamber front chamber 10 in firing chamber rear chamber 11 and becomes inflammable mixture through rotor air outlet 18 of calming the anger, inflammable mixture promotes acting rotor 3 further with high-temperature high-pressure fuel gas in firing chamber front chamber 10 together burning expansion and rotates, described acting rotor shaft 6 end output power.The pump type of blade described in the present embodiment rotor 51 and previous stage blade pump type rotor 52 of calming the anger of calming the anger forms two-stage blade pump type and to calm the anger rotor, improve the compression ratio of rotor output squeezing air of calming the anger, pressurized gas pressure in further raising firing chamber rear chamber 7, gaseous-pressure in further raising firing chamber front chamber 6, is conducive to the Thorough combustion of fuel.

Figure 20, Figure 21 shows this programme the 9th specific embodiment, can be found out by accompanying drawing, internal combustion engine shown in the present embodiment is by body 1, centrifugal rotor 2 of calming the anger, blade pump type calm the anger rotor 51 and non-turbine-type acting rotor 3 form, described non-turbine-type acting rotor 3 is unshrouded impeller structures, described blade pump type rotor 51 of calming the anger is arranged on blade pump type oval in body 1 and calms the anger in rotor 51 chamber, described centrifugal calm the anger rotor 2 and impeller type acting rotor 3 be arranged on body 1 inner cylindrical acting rotor 3 chamber in, described blade pump type calms the anger rotor 51 and centrifugal rotor 2 and the impeller type acting rotor 3 of calming the anger all in body 1 on the same axis line, described blade pump type rotor 51 of calming the anger is arranged on and calms the anger on rotor shaft 5 for final stage rotor of calming the anger, described centrifugal rotor 2 of calming the anger is arranged on previous stage and calms the anger on rotor shaft 55, described acting rotor 3 is arranged on acting rotor shaft 6, described calm the anger rotor shaft 5 and previous stage rotor shaft 55 of calming the anger is coaxial connections, described rotor shaft 5 of calming the anger connects with acting rotor shaft 6 through planetary gear set 32, described planetary gear set 32 there is planetary gear set control gear 33, described body 1 has above previous stage rotor suction port 53 of calming the anger to communicate with centrifugal rotor 2 of calming the anger, described previous stage rotor air outlet 54 of calming the anger is communicated with rotor suction port 4 of calming the anger, described suction port 4 is communicated with blade pump type rotor 51 of calming the anger, described rotor air outlet 18 of calming the anger there is gas storage valve 19, described gas storage valve 19 is communicated with the outer caisson 20 of body 1, described acting rotor 3 impeller upper blade 28 is fixed on wheel body not with the contact of chamber wall, described previous stage is calmed the anger rotor shaft 55, calm the anger on rotor shaft 5 and acting rotor shaft 6 and bearing 7 is housed in body 1 spacing wall, throat less chamber is had in body 1 above described acting rotor 3 chamber, described firing chamber front chamber 10 front end is communicated with the suction port 21 of acting rotor 3, the air outlet 25 of described acting rotor 3 communicates with air outlet flue 26, the air flue 36 outer air outlet flue 36 of described air outlet 25 with annular gas tank 34 connection on the sidewall of acting rotor 3 chamber there is gas exhausting valve 38, described air flue 36 there is air valve 37, described planetary gear set 32 is identical with planetary gear set control gear 33 with planetary gear set 32 described in the second embodiment with planetary gear set control gear 33, described acting rotor 3 follows the acting rotor 3 described in the basic structure of firing chamber and same 8th embodiment of working principle identical with firing chamber, here no longer describe in detail, rotor of calming the anger in the present embodiment forms the coaxial gas pressure mechanism of mixing two-stage by centrifugal calm the anger rotor 2 and blade type pump type rotor 51 of calming the anger, mixing two stage compressor structure can utilize the performance characteristic of various forms of rotor of calming the anger to improve working rotor efficiency of calming the anger further better, effective raising is calmed the anger the pressurized gas pressure of rotor air outlet 18.

Figure 20, Figure 22 shows this programme the tenth specific embodiment, can be found out by accompanying drawing, internal combustion engine shown in the present embodiment is by body 1, centrifugal rotor 2 of calming the anger, blade pump type calm the anger rotor 51 and non-turbine-type acting rotor 3 form, described non-turbine-type acting rotor 3 is unshrouded impeller structures, described blade pump type rotor 51 of calming the anger is arranged on blade pump type oval in body 1 and calms the anger in rotor 51 chamber, described centrifugal calm the anger rotor 2 and impeller type acting rotor 3 be arranged on body 1 inner cylindrical acting rotor 3 chamber in, described blade pump type calms the anger rotor 51 and centrifugal rotor 2 and the impeller type acting rotor 3 of calming the anger all in body 1 on the same axis line, described blade pump type rotor 51 of calming the anger is arranged on and calms the anger on rotor shaft 5 for final stage rotor of calming the anger, described centrifugal rotor 2 of calming the anger is arranged on previous stage and calms the anger on rotor shaft 55, described acting rotor 3 is arranged on acting rotor shaft 6, described rotor shaft 5 one-level in front of planetary gear set 32 of calming the anger rotor shaft 55 of calming the anger connects, described rotor shaft 5 of calming the anger connects with acting rotor shaft 6 through planetary gear set 32, described planetary gear set 32 there is planetary gear set control gear 33, described body 1 has above previous stage rotor suction port 53 of calming the anger to communicate with centrifugal rotor 2 of calming the anger, described previous stage rotor air outlet 54 of calming the anger is communicated with rotor suction port 4 of calming the anger, described suction port 4 is communicated with blade pump type rotor 51 of calming the anger, described rotor air outlet 18 of calming the anger there is gas storage valve 19, described gas storage valve 19 is communicated with the outer caisson 20 of body 1, described acting rotor 3 impeller upper blade 28 is fixed on wheel body not with the contact of chamber wall, described previous stage is calmed the anger rotor shaft 55, calm the anger on rotor shaft 5 and acting rotor shaft 6 and bearing 7 is housed in body 1 spacing wall, throat less chamber is had in body 1 above described acting rotor 3 chamber, described firing chamber front chamber 10 front end is communicated with the suction port 21 of acting rotor 3, the air outlet 25 of described acting rotor 3 communicates with air outlet flue 26, the air flue 36 outer air outlet flue 36 of described air outlet 25 with annular gas tank 34 connection on the sidewall of acting rotor 3 chamber there is gas exhausting valve 38, described air flue 36 there is air valve 37, described planetary gear set 32 is identical with planetary gear set control gear 33 with planetary gear set 32 described in the second embodiment with planetary gear set control gear 33, described acting rotor 3 follows the acting rotor 3 described in the basic structure of firing chamber and same 8th embodiment of working principle identical with firing chamber, here no longer describe in detail, rotor of calming the anger in the present embodiment forms mixing two stage compressor structure by centrifugal calm the anger rotor 2 and blade type pump type rotor 51 of calming the anger, mixing two stage compressor structure can utilize the performance characteristic of various forms of rotor of calming the anger to improve working rotor efficiency of calming the anger further better under the flexible allotment of planetary gear set 32 pairs of rotating speeds, effective raising is calmed the anger the pressurized gas pressure of rotor air outlet 18.

Figure 20, Figure 23 shows this programme the 11 specific embodiment, can be found out by accompanying drawing, internal combustion engine shown in the present embodiment to be calmed the anger rotor 56 by turbine-type, previous stage turbine-type is calmed the anger rotor 56 ', front secondary turbine-type calm the anger rotor 56 〞 and non-turbine-type acting rotor 3 and body 1 form, described turbine-type rotor 56 of calming the anger is arranged on and calms the anger on rotor shaft 5 for final stage rotor of calming the anger, previous stage turbine-type rotor 56 ' of calming the anger is arranged on previous stage and calms the anger on rotor shaft 55, described front secondary turbine-type rotor 56 〞 that calms the anger is arranged on front secondary and calms the anger on rotor shaft 57, described acting rotor 3 is arranged on acting rotor shaft 6, described turbine-type is calmed the anger rotor 56, previous stage turbine-type is calmed the anger rotor 56 ', front secondary turbine-type calm the anger rotor 56 〞 and non-turbine-type acting rotor 3 all in body 1, same axis is arranged on respectively rotor 56 chamber of calming the anger, previous stage is calmed the anger rotor 56 ' chamber, front secondary is calmed the anger in rotor 56 〞 chamber and acting rotor 3 chamber, described acting rotor shaft 6 is with calming the anger between rotor shaft 5, one-level in front of rotor shaft 5 of calming the anger is calmed the anger between rotor shaft 55, it is all connect by planetary gear set 32 that previous stage calms the anger that secondary in front of rotor shaft 55 calms the anger between rotor shaft 57, described planetary gear set 32 there is planetary gear set control gear 33, described acting rotor 3 is unshrouded impeller structures, described impeller blade 28 is fixed on wheel body, combuster in body 1 above described acting rotor 3 chamber, described firing chamber is identical with acting rotor 3 with the firing chamber described in the 8th embodiment with acting rotor 3, described body 1 front end has front secondary rotor 56 〞 that calms the anger of secondary in front of rotor suction port 59 that calms the anger to communicate, the described front secondary rotor suction port 53 of calming the anger of one-level in front of rotor air outlet 58 of calming the anger is communicated with, calm the anger rotor air outlet 54 of described previous stage is communicated with final stage rotor suction port 4 of calming the anger, described final stage calms the anger rotor air outlet 18 with firing chamber rear chamber 11 rear end connection, described air outlet 18 there is gas storage valve 19, described gas storage valve 19 is communicated with the outer caisson 20 of body 1, described firing chamber front chamber 10 front end is communicated with the suction port 21 of acting rotor 3, the air outlet 25 of described acting rotor 3 communicates with air outlet flue 26, the air flue 36 outer air outlet flue 36 of described air outlet 25 with annular gas tank 34 connection on the sidewall of acting rotor 3 chamber there is gas exhausting valve 38, described air flue 36 there is air valve 37, to be calmed the anger rotor 56 by turbine-type in the present embodiment, previous stage turbine-type is calmed the anger rotor 56 ', front secondary turbine-type rotor 56 〞 that calms the anger forms multistage turbine formula and to calm the anger rotor, utilize planetary gear set 32 and planetary gear set control gear 33 can flexible modulation multistage turbine formula calm the anger rotor at different levels between and final stage calm the anger rotor 56 with the rotating ratio between acting rotor 3, further play and utilize multistage turbine formula to calm the anger the advantage of rotor.

Figure 20, Figure 24 shows this programme the 12 specific embodiment, can be found out by accompanying drawing, internal combustion engine shown in the present embodiment is by centrifugal rotor 2 of calming the anger, turbine-type is calmed the anger rotor 56, previous stage turbine-type is calmed the anger rotor 56 ', front secondary turbine-type calm the anger rotor 56 〞 and non-turbine-type acting rotor 3 and body 1 form, described centrifugal rotor 2 of calming the anger is arranged on and calms the anger on rotor shaft 5 for final stage rotor of calming the anger, turbine-type rotor 56 of calming the anger is arranged on previous stage and calms the anger on rotor shaft 55, described previous stage turbine-type rotor 56 ' of calming the anger is arranged on front secondary and calms the anger on rotor shaft 57, described front secondary turbine-type rotor 56 〞 that calms the anger is arranged on first three level and calms the anger on rotor shaft 60, described acting rotor 3 is arranged on acting rotor shaft 6, described centrifugal rotor 2 of calming the anger, turbine-type is calmed the anger rotor 56, previous stage turbine-type is calmed the anger rotor 56 ', front secondary turbine-type calm the anger rotor 56 〞 and non-turbine-type acting rotor 3 all same axis is arranged on respectively centrifugal rotor 2 chamber of calming the anger in body 1, to calm the anger rotor 56 chamber, previous stage is calmed the anger rotor 56 ' chamber, front secondary is calmed the anger in rotor 56 〞 chamber and acting rotor 3 chamber, described acting rotor shaft 6 is with calming the anger between rotor shaft 5, one-level in front of rotor shaft 5 of calming the anger is calmed the anger between rotor shaft 55, previous stage calm the anger secondary in front of rotor shaft 55 calm the anger between rotor shaft 57 and front secondary to calm the anger in front of rotor shaft 57 that three grades are calmed the anger between rotor shaft 60 be all connect by planetary gear set 32, described planetary gear set 32 there is planetary gear set control gear 33, described acting rotor 3 is unshrouded impeller structures, described impeller blade 28 is fixed on wheel body, combuster in body 1 above described acting rotor 3 chamber, described firing chamber is identical with acting rotor 3 with the firing chamber described in the 8th embodiment with acting rotor 3, described body 1 front end has first three level rotor 56 〞 that calms the anger of secondary turbine-type in front of rotor suction port 61 that calms the anger to communicate, first three level described rotor suction port 59 of calming the anger of secondary turbine-type in front of rotor air outlet 62 of calming the anger is communicated with, calm the anger rotor air outlet 58 of described front secondary turbine-type is communicated with turbine-type rotor suction port 53 of calming the anger, calm the anger rotor 56 air outlet 54 of described turbine-type is communicated with centrifugal rotor 2 suction port 4 of calming the anger, described final stage calms the anger rotor air outlet 18 with firing chamber rear chamber 11 rear end connection, described air outlet 18 there is gas storage valve 19, described gas storage valve 19 is communicated with the outer caisson 20 of body 1, described firing chamber front chamber 10 front end is communicated with the suction port 21 of acting rotor 3, the air outlet 25 of described acting rotor 3 communicates with air outlet flue 26, the air flue 36 outer air outlet flue 36 of described air outlet 25 with annular gas tank 34 connection on the sidewall of acting rotor 3 chamber there is gas exhausting valve 38, described air flue 36 there is air valve 37, in the present embodiment by centrifugal rotor 2 of calming the anger, turbine-type is calmed the anger rotor 56, previous stage turbine-type rotor 56 ' and front secondary turbine-type rotor 56 〞 that calms the anger that calms the anger jointly forms hybrid multi-stage and to calm the anger rotor, utilize planetary gear set 32 and planetary gear set control gear 33 pairs of hybrid multi-stages to calm the anger between each rotor of rotor and hybrid multi-stage calm the anger rotor with acting rotor 3 between connect, hybrid multi-stage can be regulated and controled more flexibly calm the anger between rotor rotor at different levels and with the rotating ratio between acting rotor 3, make pressure-combustion coupling better.

Figure 20, Figure 25 shows this programme the 13 specific embodiment, can be found out by accompanying drawing, internal combustion engine shown in the present embodiment is by body 1, front secondary turbine-type acting rotor 56 〞, previous stage turbine-type is calmed the anger rotor 56 ', turbine-type is calmed the anger rotor 56, calm the anger rotor 51 and non-turbine-type acting rotor 3 of centrifugal calm the anger rotor 2 and blade pump type is formed, described blade pump type rotor 51 of calming the anger is arranged on and calms the anger on rotor shaft 5 for final stage rotor of calming the anger, described centrifugal rotor 2 of calming the anger is arranged on previous stage and calms the anger on rotor shaft 55, described turbine-type rotor 56 of calming the anger is arranged on front secondary and calms the anger on rotor shaft 57, previous stage turbine-type rotor 56 ' of calming the anger is arranged on first three level and calms the anger on rotor shaft 60, described front secondary turbine-type rotor 56 〞 that calms the anger is arranged on front level Four and calms the anger on rotor shaft 63, described acting rotor 3 is arranged on acting rotor shaft 6, described blade pump type is calmed the anger rotor 51, centrifugal rotor 2 of calming the anger, turbine-type is calmed the anger rotor 56, previous stage turbine-type is calmed the anger rotor 56 ', calm the anger rotor 56 〞 and non-turbine-type acting rotor 3 of front secondary turbine-type all same axis is arranged on respectively blade pump type in body 1 and calms the anger rotor 51 chamber, centrifugal rotor 2 chamber of calming the anger, to calm the anger rotor 56 chamber, previous stage is calmed the anger rotor 56 ' chamber, front secondary is calmed the anger in rotor 56 〞 chamber and acting rotor 3 chamber, described acting rotor shaft 6 is with calming the anger between rotor shaft 5, one-level in front of rotor shaft 5 of calming the anger is calmed the anger between rotor shaft 55, previous stage secondary in front of rotor shaft 55 of calming the anger is calmed the anger between rotor shaft 57, front secondary to calm the anger in front of rotor shaft 57 three grades calm the anger between rotor shaft 60 and first three level to calm the anger that level Four in front of rotor shaft 60 calms the anger between rotor shaft 63 be all connect by planetary gear set 32, described planetary gear set 32 there is planetary gear set control gear 33, described acting rotor 3 is unshrouded impeller structures, described impeller blade 28 is fixed on wheel body, combuster in body 1 above described acting rotor 3 chamber, described firing chamber is identical with acting rotor 3 with the firing chamber described in the 8th embodiment with acting rotor 3, described body 1 front end has front level Four rotor 56 〞 that calms the anger of secondary turbine-type in front of rotor suction port 64 that calms the anger to communicate, described front level Four three grades of rotor suction ports 61 of calming the anger in front of rotor air outlet 65 of calming the anger are communicated with, first three level described rotor suction port 59 of calming the anger of secondary in front of rotor air outlet 62 of calming the anger is communicated with, the front secondary rotor suction port 53 of calming the anger of one-level in front of rotor air outlet 58 of calming the anger is communicated with, described previous stage rotor air outlet 54 of calming the anger is communicated with rotor suction port 4 of calming the anger, described final stage calms the anger rotor air outlet 18 with firing chamber rear chamber 11 rear end connection, described rotor air outlet 18 of calming the anger there is gas storage valve 19, described gas storage valve 19 is communicated with the outer caisson 20 of body 1, described firing chamber front chamber 10 front end is communicated with the suction port 21 of acting rotor 3, the air outlet 25 of described acting rotor 3 communicates with air outlet flue 26, the air flue 36 outer air outlet flue 36 of described air outlet 25 with annular gas tank 34 connection on the sidewall of acting rotor 3 chamber there is gas exhausting valve 38, described air flue 36 there is air valve 37, to be calmed the anger rotor 51 by blade pump type in this specific embodiment, centrifugal rotor 2 of calming the anger, turbine-type is calmed the anger rotor 56, previous stage turbine-type rotor 56 ' and front secondary turbine-type rotor 56 〞 that calms the anger that calms the anger jointly forms hybrid multi-stage and to calm the anger rotor, utilize planetary gear set 32 and planetary gear set control gear 33 pairs of hybrid multi-stages to calm the anger between each rotor of rotor and hybrid multi-stage calm the anger rotor with acting rotor 3 between connect, hybrid multi-stage can be regulated and controled more flexibly calm the anger between rotor rotor at different levels and with the rotating ratio between acting rotor 3, make pressure-combustion coupling better, the pressurized air of more high compression ratio can be provided, suitably the different conditional request required for various fuel combustion is adapted in the adjustment position of piston 8 in firing chamber by firing chamber rear chamber 7 inner carrier position controller 10, reach a machine multi fuel object.

By finding out describing of above 13 specific embodiments, the application can have many changes to be not limited only to above 13 specific embodiments, can exchange between above 13 specific embodiments with or without, mutually exchange, as can by first, second, 3rd, 4th, 5th, 6th, acting rotor in 7th embodiment is with the 8th, 9th, tenth, 11, 12, the rotor that does work in 13 embodiment exchanges, and can also reconfigure, and also has described acting rotor can be one, two, or the multiple acting rotor of two or more, also have, it also can be that the private firing chamber of each acting rotor can also divide into groups to use firing chamber that described multiple acting rotor can share a firing chamber, described in rotor of calming the anger can be centrifugal turbocompressor, blade pump type gas compressor, turbine-type hinge gas compressor also can be that other form being applicable to this programme is calmed the anger rotor, described in rotor of calming the anger can be one-level, two-stage and the above multistage compressor structure of two-stage, as multistage turbine gas compressor, multistage blade gas compressor etc., described in calm the anger rotor can also be various ways gas compressor form hybrid multi-stage gas pressure mechanism, be final stage as made primary centrifugal turbocompressor with turbine hinge formula gas compressor, centrifugal turbocompressor is primary blades pump type gas compressor is the mixed construction such as middle final stage, described multistage compressor structure or hybrid multi-stage gas pressure mechanism at different levels between can be coaxial pattern also can be by the split axle pattern that planetary gear set connects can also be that selectively to use planetary gear set to carry out connection coaxial, split axle mixed mode, described planetary gear set can be single planetary gear set structure also can be two or more multiple planetary gear set structures, described camshaft, gas storage control valve, caisson, flameholder and gas exhausting valve can save.Above all changes are all within the application's protection domain.

Claims (9)

1. an internal combustion engine, primarily of body, to calm the anger rotor, acting rotor and fuel supplying device, ignition mechanism is formed, rotor of calming the anger is arranged on respectively with acting rotor calms the anger in rotor chamber and acting rotor chamber, acting rotor and calm the anger between rotor and have interval body wall and spring bearing, suction port is had to follow rotor of calming the anger to communicate before body, it is characterized in that: described in rotor of calming the anger be connected with acting rotor diaxon on same axis, described acting rotor is non-turbine-type blade wheel structure, combuster in body above acting rotor, and firing chamber is cylindrical shape, the cylindrical piston matched with circular diameter in firing chamber is had in firing chamber, described cylindrical piston periphery there is seal ring, described cylindrical piston is divided into former and later two chambers firing chamber, described cylindrical piston can slide in the front and back chamber of firing chamber, there is fumarole at described cylindrical piston center, described fumarole center is built with fuel injector, described fuel injector can be axially movable in fumarole, spring is had in described cylindrical piston rear end firing chamber rear chamber, described spring rear end has piston position controller, telescopic pipe is had in described spring ring, described telescopic pipe front end communicates with fuel injector, telescopic pipe rear end is through piston position controller, body communicates with fuel supplying device, described firing chamber rear chamber rear end is communicated with rotor air outlet of calming the anger, described firing chamber front chamber front end is communicated with acting rotor suction port, described acting rotor suction port is provided with ignition mechanism, the air outlet of described acting rotor communicates with air outlet flue at the another side that suction port is corresponding.

2. a kind of internal combustion engine according to claim 1, it is characterized in that: described acting rotor chamber is circular, in described acting rotor chamber, impeller has with blade with wide tongue piece between adjacent two blades, a limit of described tongue piece with a blade top margin in adjacent two blades through the Viability connection of movable axis, described tongue piece is that the blade face of its another edge another blade adjacent of axle center slides up and down in scope between 0-90 degree with movable axis, its top dead center is no more than the corresponding blade top margin slided, its radian of blade face camber corresponding to the sliding edge of described tongue piece and the slip radian of tongue piece sliding edge match, active edges adjacent two blades when top dead center of described tongue piece, tongue piece, a rotor cavity is formed between the wheel body of impeller, on described acting rotor chamber sidewall, there is annular gas tank the sub-cavity bottom corresponding part of transfer, described annular gas tank communicates with acting rotor air outlet through air flue, described air flue there is air valve, communicate with corresponding annular gas tank on acting rotor chamber sidewall bottom described rotor cavity.

3. a kind of internal combustion engine according to claim 1, it is characterized in that: described acting rotor chamber is oval, blade is had to slide from inside to outside in the wheel body axial notch of described impeller, vane hole is had in described blade, roller is had to follow the contact of oval acting rotor chamber inner headed face in described blade end face groove, in described acting rotor chamber, impeller has with blade with wide tongue piece between adjacent two blades, described tongue piece is in active string by concave volume and convex body to insert and form, in described concave volume, convex body top end there is spring, a limit of described tongue piece with a blade top margin in adjacent two blades through the Viability connection of movable axis, described tongue piece is that the blade face of its another edge another blade adjacent of axle center slides up and down in scope between 0-90 degree with movable axis, its top dead center is no more than the corresponding blade top margin slided, the slip radian of its radian of blade face camber corresponding to the sliding edge of described tongue piece and the sliding edge of tongue piece matches, active edges adjacent two blades when top dead center of described tongue piece, tongue piece, a rotor cavity is formed between the wheel body of impeller, described vane hole one end communicates with bottom impeller cavity with the other end that communicates bottom axial notch, described acting rotor chamber sidewall there is annular gas tank with corresponding part bottom axial notch, described annular gas tank communicates with acting rotor air outlet through air flue, described air flue there is air valve, communicate with corresponding annular gas tank on acting rotor chamber sidewall bottom described axial notch, described rotor cavity communicates with bottom axial notch through vane hole.

4. a kind of internal combustion engine according to any one of claim 1,2,3, is characterized in that: described acting rotor is two.

5. a kind of internal combustion engine according to any one of claim 1,2,3, is characterized in that: described acting rotor is multiple.

6. a kind of internal combustion engine according to any one of claim 1,2,3, is characterized in that: described in rotor of calming the anger be the two stage compressor structure that two rotors are formed.

7. a kind of internal combustion engine according to any one of claim 1,2,3, is characterized in that: described in calm the anger rotor be multiple rotor form multistage compressor structure.

8. a kind of internal combustion engine according to any one of claim 1,2,3, is characterized in that: described in calm the anger rotor be multiple rotor form hybrid multi-stage gas pressure mechanism.

9. a kind of internal combustion engine according to any one of claims 1 to 3, it is characterized in that: described in calm the anger on rotor air outlet and have gas storage control valve, gas storage control valve connects with the outer caisson of body, guiding piece is had in the center puff prot of described piston, described acting rotor suction port there is flameholder, there is camshaft at suction port place, described air outlet flue has gas exhausting valve, described acting rotor with calm the anger rotor and do work rotor and rotor of calming the anger at different levels between axle on have planetary gear set and planetary gear set control gear.